Plane & Pilot
Thursday, April 1, 2004

1974 Piper Pathfinder N57347



piper
Engine make/model:Lycoming O-540-B4B5
Horsepower@altitude: 235@SL
Horsepower for takeoff:235
TBO hrs.:
2000
Fuel type:100/100LL
Propeller type/diameter:
Hartzell CS
Landing gear type:
Tri/Fixed
Max ramp weight (lbs.):3000
Gross weight (lbs.): 3000
Landing weight (lbs.):3000
Empty weight, std. (lbs.): 1550
Useful load, std. (lbs.): 1450
Payload, full std. fuel (lbs.):
958
Usable fuel (gals.): 82
Oil capacity (qts.):12
Wingspan: 32 ft.
Overall length: 24 ft.
Height: 7 ft. 10 in.
Wing area (sq. ft.):170
Wing loading (lbs./sq. ft.):
17.6
Power loading (lbs./hp.):
12.8
Wheel size (in.):
6.00 x 6
Seating capacity: 4
Cabin doors:
1
Cabin width (in.): 44
Cabin height (in.): 47
Baggage capacity (lbs.):200
 
PERFORMANCE
Cruise speed (kts.):  
75% power: 133
65% power: 127*
55% power:
122*
  
Max range (w/ reserve) (nm):  
75% power:
718**
65% power:
813**
55% power:
939**
  
Fuel consumption (gph):
 
75% power: 12.8**
65% power:11.1**
55% power:
9.4**
  
Estimated endurance (65%) (hrs): 6.4**
Vs (kts.):
57
Vso (kts.):
52
Best rate of climb (SL fpm): 800
Best rate of climb, 8000 ft. (fpm):
400*
Service ceiling (ft.): 13,550
Takeoff ground roll (ft.): 850
Takeoff over 50-ft. obstacle (ft.):1410
Landing ground roll (ft.): 1040
Landing over 50-ft. obstacle (ft.):
1740
 
*estimated
**calculated
Sources: Aircraft Bluebook Price Digest, Jane’s All The World’s Aircraft





Labels: Specs

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